NASA-STD-5009C:2023
Current
The latest, up-to-date edition.
Nondestructive Evaluation Requirements for Fracture Critical Metallic Components
English
03-08-2023
This NASA Technical Standard establishes the nondestructive evaluation (NDE) requirements for any NASA system or component, flight or ground, where fracture control and a quantitative demonstration of probability of detection (POD) are required.
| DocumentType |
Standard
|
| Pages |
54
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Current
|
| Supersedes |
| MIL-HDBK-1823 Revision A:2009 | Nondestructive Evaluation System Reliability Assessment |
| SAE AS4787A | Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware |
| ASTM E 1742/E1742M : 2018 | Standard Practice for Radiographic Examination |
| SAE AMS2647G | Fluorescent Penetrant Inspection Aircraft Structures and Engine Component Maintenance |
| ASTM E 1417/E1417M : 2021 | Standard Practice for Liquid Penetrant Testing |
| ASTM E 2375 : 2022 | Standard Practice for Ultrasonic Testing of Wrought Products |
| ASTM E 1444/E1444M : 2021 | Standard Practice for Magnetic Particle Testing for Aerospace |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| ASTM E 164 : 2019 | Standard Practice for Contact Ultrasonic Testing of Weldments |
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